Registered owner
Air Methods LLC
Owner type
LLC
Serial number
0324
Year built
2004
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
October 26, 2004
Certificate issued
May 22, 2014
Expires
May 31, 2027
Mode S code
A08A19

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada PW206B model are included below.

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Airworthiness directives that may apply · 51

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

2000In forceSuperseded2026
ADs by the year they took effect: 64 ADs
20001
20042
20082
20092
20124
20138
20145
20151
20162
20171
20182
20194
20201
202111
20226
20244
20253
20265
See all 66 ADs

Information bulletins that may apply · 3

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N134AMMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Eurocopter Deutschland EC 135 P2 aircraft

FAA incident reports

No FAA accident or incident reports matched to N134AMMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Eurocopter Deutschland EC 135 P2 aircraft

Service difficulty reports · 8

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR QMLA2025012020005Windscreen · crackedPILOTS' WINDSCREEN CRACKED WHILE RETURNING TO BASE.Jan 20, 2025 · N134AM · Urocop EC135P2 · Flight Compartment WindowsSDR 2A6R2022081564503Deck Plate · crackedDURING INSPECTION, FOUND A CRACK ON THE TRANSMISSION DECK 0.9 INCH BY 1 INCH AT STATION 4170 MM WL 2760 MM RBL 40 MMAug 15, 2022 · N134AM · Urocop EC135P2 · Fuselage Main, StructureSDR 2A6R2022080564503None · noneDURING A SCHEDULED INSPECTION OF FRAME 5 REQUIRED BY ASB21-01, DAMAGE WAS DISCOVERED AT FS 4,709 MM THE DAMAGE IS ADJACENT TO THE MEDICAL WALL ATTACH FITTINGS.Aug 5, 2022 · N134AM · Urocop EC135P2 · Fuselage Structure (General)SDR 2A6R2022080564502Bulkhead · corrodedDURING A 1000 HOUR AIRFRAME INSPECTION FOUND CORROSION AT THE FS 3150 BULKHEADAug 5, 2022 · N134AM · Urocop EC135P2 · Fuselage Main, BulkheadSDR 2A6R2022080564501Keelbeam · corrodedDURING 1000 HOUR AIRFRAME INSPECTION FOUND CORROSION ON L/H KEEL BEAM CAP BENEATH THE EDGE OF THE COCKPIT FLOORAug 5, 2022 · N134AM · Urocop EC135P2 · Fuselage Main, KeelSDR 2A6R20190415525Frame · crackedDURING THE COURSE OF MAINTENANCE, A CRACK WAS FOUND IN THE RH FRAME 5 U-PROFILE CHANNEL, JUST BELOW WHERE THE AVIONICS SHELF ATTACHES.Apr 15, 2019 · N134AM · Urocop EC135P2 · Fuselage Main, FrameSDR QMLA2016110216121Arm · cracked#1 STATOR ARM CRACKED AT LH UPPER CORNER. THIS AIRCRAFT REMAINS OOS AT THE TIME OF THIS SUBMISSION.Nov 2, 2016 · N134AM · Urocop EC135P2 · Rotorcraft Tail BoomSDR QMLA2013081413116Master Box · failedPILOT REPORTED WHILE IN CRUISE, THE AIR CONDITIONING SUDDENLY STOPPED BLOWING AIR. CYCLED AIR CONDITIONING CONTROL SWITCH AND CHECKED THE CIRCUIT BREAKER. NOTICED THAT BOTH "BUSS TIE OPEN" LIGHTS WERE ON, AND THEN A STRONG ELECTRICAL BURNING SMELL BEGAN TO Aug 14, 2013 · N134AM · Urocop EC135P2 · DC Power Distribution System

STCs that may be installed · 72

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 72 STCs